Features

Monitor and Control of all the UAV parameters in all the phases of flight

External Pilot interface

Payload control and monitoring

Automatic takeoff and landing system (ATOL) interface

Health monitoring of UAV systems, GCS, GDT, EP and SATCOM

Recording of UAV and Payload data

Synchronization of all the UAV parameters

Dissemination of UAV sensors data to services in required format

Replay of recorded information

Post flight analysis

Inter and Intra communications

Data Link

Features

Anti-Jam/clear command up-link

Integrated payload & telemetry down-link

Real time, full motion EO & IR digital compressed video

Multiplexed user data for SAR/MPR/ESM

Full duplex voice link for ATC

User selectable COMSEC (uplink & downlink)

Steerable on board directional antenna

Monopulse ground tracking antenna (azimuth)

Shipborne Terminals for maritime surveillance

LOS & SATCOM operation

Get-U-Home Panel

The Get-U-HOME panel is a LCD type display for providing essential flight parameters. The following parameters are displayed on the LCD panel

Indicated Air Speed (IAS)

Vertical Speed (VSI)

Mach number

Angle of Attack (AOA)

Magnetic Heading

Altitude

Multifunction Keyboard

The Multifunction keyboard is a combined control and display unit. It comprises of alphanumeric keyboard and a LCD dot matrix display and is used for data entry and management of the various aircraft systems

MFK controls the Power ON / OFF of Radio Altimeter, V/UHF, IFFT (Transponder) through the keyboard

MFK also performs the Data loading, Selection and Display of relevant page information, Modification and validation of parameters and Clock Management functions. On ground, the MFK performs the following functions: Form an interface for pilot's dialogue during initialization phase of the aircraft. Displays maintenance (MNT) and internal coded data (ICD) after the flight

Multifunction Rotary Switch

The Multifunctional Rotary Switch, situated in the instrument panel of LCA, performs two main functions.

Modification of parameters

Display of time

The unit has a twelve position rotary switch to select the parameter and a concentric optical encoder to modify that parameter.

The stopwatch display is controlled by a toggle switch.

A display ON/OFF switch controls the display on HUD. The unit receives inputs from the Video Switching Unit (VSU), the display processors and Multifunction keyboard.

Engine Fuel Indicator

The engine fuel indicator is a LCD based cockpit display unit that indicates the essential parameters of the Engine and Fuel systems in the Aircraft to the Pilot.

Pylon Interface Box

FEATURES

PIB is a Weapon control system which is part of Stores Management System (SMS) of the aircraft

It control the release of weapons under the control of master weapon computer and cockpit discrete signals through dual redundant architecture

Air Data Computer

Air Data Computer (ADC) is part of flight control system of the aircraft. It performs air data computation like atmospheric pressure, temperature and angle of attack by taking input from air data sensors like pressure transducers, temperature sensor a nd ang le of attack sensor.

Data Link Airborne

DATA LINK is an onboard system for

HELICOPTERS

AIRCRAFTS

ROLE

Data Link is aimed at integrating the tactical pictures and messages between units on air and ashore in a fast, reliable and secure manner.

FEATURES

First of kind cPCI COTS hardware certified to aviation standards for any armed force

Information of unit position, air, surface, sub surface and special tracks position ESM bearing, aircraft status, OT Targeting Message, order Message etc. are available over the network

Tracks of Air, Surface, Sub surface, Special Tracks can be exchanged amongst different platforms

Function Sensor Display Unit

SMART, Spurt Message Alphanumeric Radio Terminal is a Data Communication Terminal for field use. The terminal provides reliable burst transmission capability to reduce radio channel occupancy time with reduction in probability of interference and jamming.

FEATURES

The Function sensor display unit provides an interactive visual interface between the pilot and the avionics system of the aircraft

FSDU will receive the commands from tasks mission computer and execute as per the requirements

FSDU has 15 keys on its front panel for selection of different functions and sensors. Corresponding to each key, three programmable legends are displayed on the LCD panel to indicate the aircraft function/sensor configuration along with their selected/deselected status

Stores Interface Box

The Stores Interface Box (weapon computer) is front-end weapon management computer based on open architecture concept. It is part of weapon control system of the aircraft and controls Pylon Interface Boxes. It controls Pylon Interface Boxes based on high level commands received from open architecture computer over 1553B bus.

Digital Flight Control Computer

DFCC is an on board computer used for the flight control functions of the Aircraft The on board computer has quadraplex construction. Each channel has got Multi layer Board which employ SMD components. All the PCBs are interconnected through the mother board, which is of polyamide material.

FEATURES

Processes the various transducer signals and discrete related to flight control in the Aircraft

Provides the basic hardware interface, which controls the Computer

Converts the 28V dc input from the Aircraft into regulated voltage for use by internal PCBs

All the hardware interfaces of analog, digital and power supply cards are accessed by software to a valid address

Head Up Display

Head Up Display displays flight information of several selectable modes in collimated form so that a pilot can view this information superimposed on his view of the outside world without having to change his line of sight or visual accommodation. The pilot is thus able to fly the aircraft 'Head-up' thereby reducing workload and enhancing his weapon aiming capability.

FEATURES

High reliability (MTBF of 3400 Hrs)

Wide field of view (25°)

Full readability in ambient light of 10,000 fL

Automatic brightness control

Compact in size

Customer tailored Up-Front Control Panel

Practically no sun reflection

Specifically designed for Light Combat Aircraft

Extensive Built-in-Test

Camera with automatic iris adjustment for brightness level from 10 to 10,000 fL